Call Number (LC) Title Results
Y 3.N 21/5:6/839 Rise in temperature of the charge in its passage through the inlet valve and port of an air-cooled aircraft engine cylinder / 2
Y 3.N 21/5:6/840 Tensile and Pack Compression Tests for Some Sheeets of Aluminum Alloy, 1025 Carbon Steel, and Chromium-Nickel Steel, Feb. 1940.
Tensile and pack compressive tests of some sheets of aluminum alloy, 1025 carbon steel, and chromium-nickel steel / 		3
Y 3.N 21/5:6/841 The photoviscous properties of fluids /
The Photoviscous properties of fluids / 		2
Y 3.N 21/5:6/842 Tidewater and weather-exposure tests on metals used in aircraft.
Tidewater and weather-exposure tests on metals used in aircraft - II / 		2
Y 3.N 21/5:6/843 A Summary of Results of Various Investigations of the Mechanical Properties of Aluminum Alloys at Low Temperatures, May 1942.
A summary of results of various investigations of the mechanical properties of aluminum alloys at low temperatures /
A Summary of results of various investigations of the mechanical properties of aluminum alloys at low temperatures / 		3
Y 3.N 21/5:6/844 Investigation of the forces acting on gliders in automobile-, pulley-, winch-, and airplane-towed flight / 2
Y 3.N 21/5:6/845 Ground effect on downwash angles and wake location / 2
Y 3.N 21/5:6/846 Bending of rectangular plates with large deflections / 2
Y 3.N 21/5:6/847 Square plate with clamped edges under normal pressure producing large deflections / 2
Y 3.N 21/5:6/848 Normal -pressure tests of circular plates with clamped edges /
Normal-pressure tests of circular plates with clamped edges / 		2
Y 3.N 21/5:6/849 Normal-pressure tests of rectangular plates / 2
Y 3.N 21/5:6/850 A preliminary investigation of the electrical structure of thunderstorms / 2
Y 3.N 21/5:6/851 Strength tests of thin-walled elliptic duralumin cylinders in pure bending and in combined pure bending and torsion / 2
Y 3.N 21/5:6/852 Effects of range of stress and of special notches on fatigue properties of aluminum alloys suitable for airplane propellers /
Effects of Range of Stress and of Special Notches on Fatigue Properties if Aluminum Alloys Suitable for Airplane Propellers. 		3
Y 3.N 21/5:6/853 Bending with large deflection of a clamped rectangular plate with length-width ratio of 1.5 under normal pressure / 2
Y 3.N 21/5:6/854 Design of tools for press-countersinking or dimpling 0.040-inch-thick 24S-T sheet / 2
Y 3.N 21/5:6/855 A method for determining the camber and twist of a surface to support a given distribution of lift /
A Method for determining the camber and twist of a surface to support a given distribution of lift / 		2
Y 3.N 21/5:6/856 Effect of rivet and spot-weld spacing on the strength of axially loaded sheet-stringer panels of 24S-T aluminum alloy / 2
Y 3.N 21/5:6/857 Improvement of fatigue life of an aluminum alloy by overstressing / 2
Y 3.N 21/5:6/858 A Comparison of the results from general tank tests of 1/6- and 1/12-full-size models of the British Singapore IIC flying boat /
A comparison of the results from general tank tests of 1/6- and 1/12-full-size models of the British Singapore IIC flying boat / 		2